Date:
December 11th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
352/04:02:44
400 1
4 1
7 1
7
N/A -0
9 0
2 196
5
000/00:09:28
800 0
1 0
2 184
8
Coasting Arc #1 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2008/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3460011
28 A = 6728213
47 meter
Y = -3178793
79 meter E =
0012919
Z = 4807471
19 I = 51
55727
XDOT = 6493
614296 Wp = 67
63936
YDOT = 3339
761870 meter/sec RA = 191
73766 deg
ZDOT = -2455
165711 TA = 46
42432
MA = 46
31715
Ha = 195
542 n
mi
Hp = 184
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11351743
04 X = 3471945
51
Y = -10429113
50 feet Y = -3140035
88 meter
Z = 15772543
28 Z = 4824308
90
XDOT = 21304
508844 XDOT = 6467
712950
YDOT = 10957
223984 feet/sec YDOT = 3412
232735 meter/sec
ZDOT = -8055
005613 ZDOT = -2423
681413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8049842
53 X = 2453592
00
Y = 13067904
04 feet Y = 3983097
15 meter
Z = 15837661
42 Z = 4827319
20
XDOT = -13932
791962 XDOT = -4246
714990
YDOT = 18236
301886 feet/sec YDOT = 5558
424815 meter/sec
ZDOT = -7932
497470 ZDOT = -2417
825229
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08345
54355434
00020000 00000-0 20000-3 0 9002
2 25544 51
6394 192
5444 0006094 76
6988 283
4853 15
71835354 16284
Satellite: ISS
Catalog Number: 25544
Epoch time: 08345
54355434 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 192
5444 deg
Eccentricity:
0006094
Arg of perigee: 76
6988 deg
Mean anomaly: 283
4853 deg
Mean motion: 15
71835354 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1628
Checksum: 318
Coasting Arc #2 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2008/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6284097
42 A = 6737422
05 meter
Y = -1904852
55 meter E =
0019847
Z = 1470233
73 I = 51
61562
XDOT = 2674
904801 Wp = 67
43524
YDOT = -4309
737961 meter/sec RA = 186
64710 deg
ZDOT = 5794
884557 TA = 308
74955
MA = 308
92675
Ha = 195
633 n
mi
Hp = 184
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20617117
53 X = -6269472
27
Y = -6249516
25 feet Y = -1975043
44 meter
Z = 4823601
47 Z = 1439740
14
XDOT = 8775
934386 XDOT = 2694
747106
YDOT = -14139
560240 feet/sec YDOT = -4279
715668 meter/sec
ZDOT = 19012
088440 ZDOT = 5807
926984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9801406
40 X = 2987468
67
Y = -19214165
36 feet Y = -5856477
60 meter
Z = 4705040
03 Z = 1434096
20
XDOT = 10983
007168 XDOT = 3347
620585
YDOT = 10315
335104 feet/sec YDOT = 3144
114140 meter/sec
ZDOT = 19062
391765 ZDOT = 5810
217010
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08346
56079545
00020000 00000-0 20000-3 0 9012
2 25544 51
6378 187
3364 0006087 81
2278 278
9573 15
71850169 16442
Satellite: ISS
Catalog Number: 25544
Epoch time: 08346
56079545 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 187
3364 deg
Eccentricity:
0006087
Arg of perigee: 81
2278 deg
Mean anomaly: 278
9573 deg
Mean motion: 15
71850169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 326
Coasting Arc #3 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2008/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1134102
65 A = 6726494
84 meter
Y = 4109008
82 meter E =
0020706
Z = -5221338
59 I = 51
60695
XDOT = -7570
672593 Wp = 93
54753
YDOT = -926
003388 meter/sec RA = 181
50353 deg
ZDOT = 917
526050 TA = 185
20704
MA = 185
22860
Ha = 195
649 n
mi
Hp = 184
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3720809
23 X = -1154601
31
Y = 13481000
08 feet Y = 4096213
02 meter
Z = -17130375
94 Z = -5226897
14
XDOT = -24838
164674 XDOT = -7564
212435
YDOT = -3038
068859 feet/sec YDOT = -1010
627081 meter/sec
ZDOT = 3010
256069 ZDOT = 880
762721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12728354
44 X = -3879602
43
Y = -5730773
90 feet Y = -1746739
89 meter
Z = -17151640
98 Z = -5227820
17
XDOT = 6554
552417 XDOT = 1997
827577
YDOT = -23121
551202 feet/sec YDOT = -7047
448806 meter/sec
ZDOT = 2867
403082 ZDOT = 873
984459
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08347
51445028
00020000 00000-0 20000-3 0 9022
2 25544 51
6364 182
4531 0006174 84
5861 275
6005 15
71851311 16590
Satellite: ISS
Catalog Number: 25544
Epoch time: 08347
51445028 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 182
4531 deg
Eccentricity:
0006174
Arg of perigee: 84
5861 deg
Mean anomaly: 275
6005 deg
Mean motion: 15
71851311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1659
Checksum: 284
Coasting Arc #4 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2008/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6723938
22 A = 6738197
71 meter
Y = -318822
02 meter E =
0016757
Z = -132543
29 I = 51
67647
XDOT = 118
694563 Wp = 119
92577
YDOT = 4773
835726 meter/sec RA = 176
39355 deg
ZDOT = -6037
108543 TA = 61
51212
MA = 61
34344
Ha = 195
605 n
mi
Hp = 184
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22060164
78 X = 6727647
48
Y = -1046004
01 feet Y = -243610
29 meter
Z = -434853
32 Z = -99869
26
XDOT = 389
417858 XDOT = 94
631267
YDOT = 15662
190701 feet/sec YDOT = 4775
029660 meter/sec
ZDOT = -19806
786558 ZDOT = -6036
589448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2116594
93 X = -645138
13
Y = 21985433
35 feet Y = 6701160
09 meter
Z = -307957
75 Z = -93865
52
XDOT = -13970
019147 XDOT = -4258
061836
YDOT = -1584
996469 feet/sec YDOT = -483
106924 meter/sec
ZDOT = -19804
395947 ZDOT = -6036
379885
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08348
53167054
00020000 00000-0 20000-3 0 9036
2 25544 51
6368 177
2457 0006140 86
8848 273
3016 15
71886020 16756
Satellite: ISS
Catalog Number: 25544
Epoch time: 08348
53167054 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 177
2457 deg
Eccentricity:
0006140
Arg of perigee: 86
8848 deg
Mean anomaly: 273
3016 deg
Mean motion: 15
71886020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1675
Checksum: 304
Coasting Arc #5 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2008/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1347475
09 A = 6726431
32 meter
Y = -3985789
96 meter E =
0009070
Z = 5240617
28 I = 51
66492
XDOT = 7492
805163 Wp = 100
44785
YDOT = -1671
435380 meter/sec RA = 171
28011 deg
ZDOT = 652
770976 TA = 343
33654
MA = 343
36633
Ha = 195
753 n
mi
Hp = 184
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4420850
03 X = -1328263
11
Y = -13076738
71 feet Y = -4000751
71 meter
Z = 17193626
24 Z = 5234117
22
XDOT = 24582
694103 XDOT = 7507
767506
YDOT = -5483
711878 feet/sec YDOT = -1587
562956 meter/sec
ZDOT = 2141
637059 ZDOT = 689
207017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13541283
09 X = 4127383
09
Y = -2838516
31 feet Y = -865179
77 meter
Z = 17168059
62 Z = 5232824
57
XDOT = 2141
818416 XDOT = 652
826253
YDOT = 24077
216106 feet/sec YDOT = 7338
735469 meter/sec
ZDOT = 2283
063594 ZDOT = 695
877784
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08349
54888275
00020000 00000-0 20000-3 0 9044
2 25544 51
6361 172
0370 0006240 91
9384 268
2493 15
71835273 16913
Satellite: ISS
Catalog Number: 25544
Epoch time: 08349
54888275 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 172
0370 deg
Eccentricity:
0006240
Arg of perigee: 91
9384 deg
Mean anomaly: 268
2493 deg
Mean motion: 15
71835273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1691
Checksum: 309
Coasting Arc #6 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2008/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6114130
85 A = 6737450
90 meter
Y = 2529518
27 meter E =
0013276
Z = -1257436
03 I = 51
73164
XDOT = -2875
813561 Wp = 61
39035
YDOT = -4059
688424 meter/sec RA = 166
14621 deg
ZDOT = 5869
500736 TA = 284
85319
MA = 285
00019
Ha = 195
567 n
mi
Hp = 184
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20059484
43 X = -6135853
56
Y = 8298944
44 feet Y = 2461025
25 meter
Z = -4125446
28 Z = -1287190
69
XDOT = -9435
083860 XDOT = -2858
716526
YDOT = -13319
187742 feet/sec YDOT = -4091
752711 meter/sec
ZDOT = 19256
892180 ZDOT = 5855
571040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6071179
71 X = -1850495
57
Y = -20818995
04 feet Y = -6345629
69 meter
Z = -4240863
57 Z = -1292615
22
XDOT = 12759
796105 XDOT = 3889
185853
YDOT = -7598
176920 feet/sec YDOT = -2315
924325 meter/sec
ZDOT = 19202
444623 ZDOT = 5852
905121
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08350
50250657
00020000 00000-0 20000-3 0 9050
2 25544 51
6361 167
1539 0006195 96
4132 263
7735 15
71891895 17063
Satellite: ISS
Catalog Number: 25544
Epoch time: 08350
50250657 = yrday
fracday
Element set: 905
Inclination: 51
6361 deg
RA of node: 167
1539 deg
Eccentricity:
0006195
Arg of perigee: 96
4132 deg
Mean anomaly: 263
7735 deg
Mean motion: 15
71891895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 305
Coasting Arc #7 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2008/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3538429
78 A = 6727629
79 meter
Y = 2909447
12 meter E =
0018468
Z = -4943491
39 I = 51
72730
XDOT = -6237
707825 Wp = 82
92197
YDOT = 3936
000789 meter/sec RA = 161
06266 deg
ZDOT = -2152
925756 TA = 166
19269
MA = 166
14211
Ha = 195
611 n
mi
Hp = 184
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11609021
57 X = 3529647
30
Y = 9545430
19 feet Y = 2948967
37 meter
Z = -16218803
78 Z = -4926322
80
XDOT = -20464
920685 XDOT = -6270
798776
YDOT = 12913
388414 feet/sec YDOT = 3866
062364 meter/sec
ZDOT = -7063
404712 ZDOT = -2183
308256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10577232
64 X = -3223940
51
Y = 10778406
10 feet Y = 3285258
18 meter
Z = -16151852
12 Z = -4923084
53
XDOT = -10201
832183 XDOT = -3109
518449
YDOT = -20749
831833 feet/sec YDOT = -6324
548743 meter/sec
ZDOT = -7181
162742 ZDOT = -2188
818404
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08351
51969675
00020000 00000-0 20000-3 0 9060
2 25544 51
6366 161
9462 0006366 99
7219 260
4663 15
71919488 17228
Satellite: ISS
Catalog Number: 25544
Epoch time: 08351
51969675 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 161
9462 deg
Eccentricity:
0006366
Arg of perigee: 99
7219 deg
Mean anomaly: 260
4663 deg
Mean motion: 15
71919488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1722
Checksum: 330
Coasting Arc #8 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2008/352/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1192867
09 A = 6726920
71 meter
Y = -4000164
88 meter E =
0009782
Z = 5266769
18 I = 51
74328
XDOT = 7224
119511 Wp = 90
39033
YDOT = -2653
173517 meter/sec RA = 157
61152 deg
ZDOT = -378
390161 TA = 3
19835
MA = 3
19210
Ha = 196
493 n
mi
Hp = 184
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3913605
95 X = -1173632
81
Y = -13123900
52 feet Y = -4013397
20 meter
Z = 17279426
44 Z = 5261020
57
XDOT = 23701
179499 XDOT = 7255
088960
YDOT = -8704
637524 feet/sec YDOT = -2572
216034 meter/sec
ZDOT = -1241
437537 ZDOT = -343
220624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3718661
68 X = -1133448
08
Y = 13210119
56 feet Y = 4026444
44 meter
Z = 17256765
36 Z = 5259862
08
XDOT = -23687
438584 XDOT = -7219
931281
YDOT = -5222
288048 feet/sec YDOT = -1591
753397 meter/sec
ZDOT = -1104
965444 ZDOT = -336
793467
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08352
21902139
00020000 00000-0 20000-3 0 9071
2 25544 51
6391 158
3694 0007366 95
4814 264
7188 15
71620020 17330
Satellite: ISS
Catalog Number: 25544
Epoch time: 08352
21902139 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 158
3694 deg
Eccentricity:
0007366
Arg of perigee: 95
4814 deg
Mean anomaly: 264
7188 deg
Mean motion: 15
71620020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1733
Checksum: 293
Coasting Arc #9 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2008/353/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5781634
70 A = 6738922
05 meter
Y = 3422721
02 meter E =
0016422
Z = -466004
29 I = 51
81024
XDOT = -2779
022971 Wp = 63
97419
YDOT = -3897
117785 meter/sec RA = 152
50210 deg
ZDOT = 6025
644180 TA = 290
97528
MA = 291
15092
Ha = 196
484 n
mi
Hp = 184
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18968617
79 X = -5817214
67
Y = 11229399
68 feet Y = 3357868
54 meter
Z = -1528885
47 Z = -494177
54
XDOT = -9117
529432 XDOT = -2764
509635
YDOT = -12785
819506 feet/sec YDOT = -3928
113796 meter/sec
ZDOT = 19769
173818 ZDOT = 6012
178638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22031399
36 X = 6715170
52
Y = 423547
16 feet Y = 129097
18 meter
Z = -1638114
53 Z = -499297
31
XDOT = 1155
677930 XDOT = 352
250633
YDOT = 14123
042816 feet/sec YDOT = 4304
703450 meter/sec
ZDOT = 19716
524825 ZDOT = 6009
596767
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08353
17282273
00020000 00000-0 20000-3 0 9088
2 25544 51
6392 153
4883 0007433 98
3495 261
8510 15
71593027 17488
Satellite: ISS
Catalog Number: 25544
Epoch time: 08353
17282273 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 153
4883 deg
Eccentricity:
0007433
Arg of perigee: 98
3495 deg
Mean anomaly: 261
8510 deg
Mean motion: 15
71593027 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1748
Checksum: 308
Coasting Arc #10 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2008/354/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3484504
37 A = 6727523
43 meter
Y = 2589695
32 meter E =
0021084
Z = -5157423
89 I = 51
79849
XDOT = -5714
281693 Wp = 87
43330
YDOT = 4943
742085 meter/sec RA = 147
41231 deg
ZDOT = -1382
254062 TA = 169
35160
MA = 169
30689
Ha = 196
446 n
mi
Hp = 184
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11432100
94 X = 3480340
86
Y = 8496375
72 feet Y = 2628638
19 meter
Z = -16920682
07 Z = -5140506
05
XDOT = -18747
643351 XDOT = -5762
423979
YDOT = 16219
626264 feet/sec YDOT = 4879
572611 meter/sec
ZDOT = -4534
954273 ZDOT = -1410
130629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5563528
85 X = -1695763
59
Y = -13196837
59 feet Y = -4022396
10 meter
Z = -16854715
61 Z = -5137317
32
XDOT = 23420
031488 XDOT = 7138
425597
YDOT = -3960
082170 feet/sec YDOT = -1207
033045 meter/sec
ZDOT = -4642
918253 ZDOT = -1415
161484
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08354
19019924
00020000 00000-0 20000-3 0 9093
2 25544 51
6401 148
2815 0007482 101
9903 258
2098 15
71634218 17642
Satellite: ISS
Catalog Number: 25544
Epoch time: 08354
19019924 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 148
2815 deg
Eccentricity:
0007482
Arg of perigee: 101
9903 deg
Mean anomaly: 258
2098 deg
Mean motion: 15
71634218 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1764
Checksum: 297
Coasting Arc #11 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2008/355/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023582
19 A = 6737292
76 meter
Y = -5032842
34 meter E =
0021521
Z = 1934470
36 I = 51
85526
XDOT = 4944
349782 Wp = 110
29854
YDOT = 1770
431895 meter/sec RA = 142
27882 deg
ZDOT = -5634
926859 TA = 48
25583
MA = 48
07202
Ha = 196
420 n
mi
Hp = 184
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13200728
97 X = 4070163
86
Y = -16511949
92 feet Y = -4987588
02 meter
Z = 6346687
52 Z = 1954129
75
XDOT = 16221
620020 XDOT = 4951
558644
YDOT = 5808
503591 feet/sec YDOT = 1825
763252 meter/sec
ZDOT = -18487
292846 ZDOT = -5610
889423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19624833
34 X = -5981649
20
Y = 7797361
69 feet Y = 2376635
84 meter
Z = 6422713
21 Z = 1957642
99
XDOT = -10720
891204 XDOT = -3267
727639
YDOT = -11717
264030 feet/sec YDOT = -3571
422076 meter/sec
ZDOT = -18393
712362 ZDOT = -5606
403528
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08355
20756540
00020000 00000-0 20000-3 0 9100
2 25544 51
6398 143
0751 0007458 105
9340 254
2644 15
71624396 17808
Satellite: ISS
Catalog Number: 25544
Epoch time: 08355
20756540 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 143
0751 deg
Eccentricity:
0007458
Arg of perigee: 105
9340 deg
Mean anomaly: 254
2644 deg
Mean motion: 15
71624396 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1780
Checksum: 290
Coasting Arc #12 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2008/356/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4911213
28 A = 6729865
96 meter
Y = -353850
15 meter E =
0015986
Z = 4577850
58 I = 51
85305
XDOT = 3285
038794 Wp = 112
02394
YDOT = -6277
299259 meter/sec RA = 137
21631 deg
ZDOT = 3024
799360 TA = 307
95158
MA = 308
09592
Ha = 196
476 n
mi
Hp = 184
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16112904
47 X = -4929130
01
Y = -1160925
68 feet Y = -408870
79 meter
Z = 15019194
83 Z = 4553948
16
XDOT = 10777
686332 XDOT = 3340
294384
YDOT = -20594
813841 feet/sec YDOT = -6240
255389 meter/sec
ZDOT = 9923
882415 ZDOT = 3040
891834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13638906
25 X = 4157138
63
Y = 8816865
14 feet Y = 2687380
49 meter
Z = 14926244
59 Z = 4549519
35
XDOT = -18668
961701 XDOT = -5690
299527
YDOT = 11894
174949 feet/sec YDOT = 3625
344525 meter/sec
ZDOT = 9985
956128 ZDOT = 3043
719428
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08356
22491969
00020000 00000-0 20000-3 0 9115
2 25544 51
6400 137
8686 0007407 109
0667 251
1297 15
71655543 17966
Satellite: ISS
Catalog Number: 25544
Epoch time: 08356
22491969 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 137
8686 deg
Eccentricity:
0007407
Arg of perigee: 109
0667 deg
Mean anomaly: 251
1297 deg
Mean motion: 15
71655543 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1796
Checksum: 313
Coasting Arc #13 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2008/357/04:07:28
800
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635796
69 A = 6734091
14 meter
Y = 5655146
65 meter E =
0011699
Z = -3282216
56 I = 51
88899
XDOT = -5952
314492 Wp = 101
93809
YDOT = 1030
169477 meter/sec RA = 132
06716 deg
ZDOT = 4753
309402 TA = 219
82559
MA = 219
91151
Ha = 196
253 n
mi
Hp = 184
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5366787
04 X = -1682967
32
Y = 18553630
74 feet Y = 5636590
84 meter
Z = -10768427
02 Z = -3290277
28
XDOT = -19528
590852 XDOT = -5986
482562
YDOT = 3379
821119 feet/sec YDOT = 963
415679 meter/sec
ZDOT = 15594
847121 ZDOT = 4724
309896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13344705
78 X = 4067466
32
Y = -13938860
03 feet Y = -4248564
54 meter
Z = -10799335
45 Z = -3291637
45
XDOT = 17914
043862 XDOT = 5460
200569
YDOT = 5185
405248 feet/sec YDOT = 1580
511519 meter/sec
ZDOT = 15482
178430 ZDOT = 4718
967986
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08357
17867947
00020000 00000-0 20000-3 0 9124
2 25544 51
6405 132
9873 0007312 112
0977 248
0961 15
71680376 18111
Satellite: ISS
Catalog Number: 25544
Epoch time: 08357
17867947 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 132
9873 deg
Eccentricity:
0007312
Arg of perigee: 112
0977 deg
Mean anomaly: 248
0961 deg
Mean motion: 15
71680376 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1811
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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